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This research discusses the case study of optimization of rocket RWX 200 motor tube with carbon fiber reinforced for 2 through 6 mm thickness. Carbon fiber is chosen due to its mechanical properties such as high strength and stiffness, and high temperature resistance, as the specification needs of t...
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| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/17080 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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id-itb.:170802017-10-09T10:19:32Z#TITLE_ALTERNATIVE# GUNAWAN PUTRA (NIM : 23607302); Pembimbing : Dr. Ir. Bambang Kismono Hadi, RONALD Indonesia Theses INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/17080 This research discusses the case study of optimization of rocket RWX 200 motor tube with carbon fiber reinforced for 2 through 6 mm thickness. Carbon fiber is chosen due to its mechanical properties such as high strength and stiffness, and high temperature resistance, as the specification needs of the rocket motor tube. Rocket motor tube is made from weaving method, while the analysis and simulation is done by assuming it as laminate with the [0/90]s stacking sequence. <br /> <br /> <br /> <br /> From the calculation and simulation, it is determined that the X stress component of the laminates is below the strength of the material, while the Y stress component is beyond the strength of the material. It can be concluded that 900 laminae in each laminates has been failed. text |
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This research discusses the case study of optimization of rocket RWX 200 motor tube with carbon fiber reinforced for 2 through 6 mm thickness. Carbon fiber is chosen due to its mechanical properties such as high strength and stiffness, and high temperature resistance, as the specification needs of the rocket motor tube. Rocket motor tube is made from weaving method, while the analysis and simulation is done by assuming it as laminate with the [0/90]s stacking sequence. <br />
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From the calculation and simulation, it is determined that the X stress component of the laminates is below the strength of the material, while the Y stress component is beyond the strength of the material. It can be concluded that 900 laminae in each laminates has been failed. |
| format |
Theses |
| author |
GUNAWAN PUTRA (NIM : 23607302); Pembimbing : Dr. Ir. Bambang Kismono Hadi, RONALD |
| spellingShingle |
GUNAWAN PUTRA (NIM : 23607302); Pembimbing : Dr. Ir. Bambang Kismono Hadi, RONALD #TITLE_ALTERNATIVE# |
| author_facet |
GUNAWAN PUTRA (NIM : 23607302); Pembimbing : Dr. Ir. Bambang Kismono Hadi, RONALD |
| author_sort |
GUNAWAN PUTRA (NIM : 23607302); Pembimbing : Dr. Ir. Bambang Kismono Hadi, RONALD |
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| url |
https://digilib.itb.ac.id/gdl/view/17080 |
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